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Volumn , Issue , 2001, Pages

Flight testing with the flutterometer

Author keywords

[No Author keywords available]

Indexed keywords

AEROSTRUCTURES; ALGORITHM AND IMPLEMENTATION; FLIGHT TESTING; FLUTTER MARGIN; FLUTTER SPEED; METHOD ANALYSIS; ON-LINE TOOLS; PAPER DOCUMENTS;

EID: 85067318370     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1654     Document Type: Conference Paper
Times cited : (2)

References (16)
  • 3
    • 0020098320 scopus 로고
    • Design for Active Flutter Suppression and Gust Load Alleviation using State-Space Aeroelastic Modeling
    • Karpel, M., Design for Active Flutter Suppression and Gust Load Alleviation using State-Space Aeroelastic Modeling, Journal of Aircraft, Vol. 19, No. 3, March 1982, pp. 221-227.
    • (1982) Journal of Aircraft , vol.19 , Issue.3 , pp. 221-227
    • Karpel, M.1
  • 6
    • 0034314729 scopus 로고    scopus 로고
    • The Flutterometer: An On-Line Tool to Predict Robust Flutter Margins
    • November-December
    • Lind, R. and Brenner M., The Flutterometer: An On-Line Tool to Predict Robust Flutter Margins, Journal of Aircraft, Vol. 37, No. 6, November-December 2000, pp. 1105-1112.
    • (2000) Journal of Aircraft , vol.37 , Issue.6 , pp. 1105-1112
    • Lind, R.1    Brenner, M.2
  • 7
    • 84894502771 scopus 로고    scopus 로고
    • Match-Point Solutions for Robust Flutter Analysis
    • submitted to, in review
    • Lind, R., Match-Point Solutions for Robust Flutter Analysis, submitted to Journal of Aircraft, in review.
    • Journal of Aircraft
    • Lind, R.1
  • 9
    • 0027205718 scopus 로고
    • The Complex Structured Singular Value
    • Packard, A. and Doyle, J., The Complex Structured Singular Value, Automática, Vol. 29, No. 1, January 1993, pp. 71-109.
    • (1993) Automática , vol.29 , Issue.1 , pp. 71-109
    • Packard, A.1    Doyle, J.2
  • 11
    • 0343743667 scopus 로고
    • Development and Analysis of Flight Flutter Prediction Methods
    • Dallax TX, AIAA-92-2101, April
    • Price, S.J. and Lee, B.H.K., Development and Analysis of Flight Flutter Prediction Methods, AIAA Dynamics Specialists Conference (Dallax TX), AIAA-92-2101, April 1992, pp. 188-200.
    • (1992) AIAA Dynamics Specialists Conference , pp. 188-200
    • Price, S.J.1    Lee, B.H.K.2
  • 12
    • 0027594303 scopus 로고
    • Evaluation and Extension of the Flutter-Margin Method for Flight Flutter Prediction
    • Price, S.J. and Lee, B.H.K., Evaluation and Extension of the Flutter-Margin Method for Flight Flutter Prediction, Journal of Aircraft, Vol. 30, No. 3, May-June 1993, pp. 395-402.
    • (1993) Journal of Aircraft , vol.30 , Issue.3 , pp. 395-402
    • Price, S.J.1    Lee, B.H.K.2
  • 14
    • 0020832479 scopus 로고
    • Evaluation of Four Subcritical Response Methods for On-Line Prediction of Flutter Onset in Wind Tunnel Tests
    • Ruhlin, C.L., Watson, J.J., Ricketts, R.H. and Doggett, R.V., Evaluation of Four Subcritical Response Methods for On-Line Prediction of Flutter Onset in Wind Tunnel Tests, Journal of Aircraft, Vol. 20, No. 10, October 1983, pp. 835-840.
    • (1983) Journal of Aircraft , vol.20 , Issue.10 , pp. 835-840
    • Ruhlin, C.L.1    Watson, J.J.2    Ricketts, R.H.3    Doggett, R.V.4
  • 16
    • 85007688839 scopus 로고
    • Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds
    • July-August
    • Zimmerman, N.H. and Weissenburger, J.T., Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds, Journal of Aircraft, Vol. 1, No. 4, July-August 1964, pp. 190-202.
    • (1964) Journal of Aircraft , vol.1 , Issue.4 , pp. 190-202
    • Zimmerman, N.H.1    Weissenburger, J.T.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.